Hinged substrate for large-aperture, lightweight, deformable mirrors
View Patent ↗An improved structure and method for building large-aperture lightweight deformable mirrors uses a hinged substrate. In addition to reduced weight, the approach provides rigidity to the mirror, which is necessary for the accurate response to actuator commands and tolerance to disturbances. No stresses are induced in the substrate due to the commanded deformation of the substrate, regardless of the magnitude of the deformation. Any stresses in the substrate structure are those induced due to forces in the face sheet, which are likely to be small using advanced nano-laminate and membrane face sheet technologies. The magnitude of the deformation (dynamic range) is limited only by the actuator stroke, and not by the stresses induced in the substrate. The design therefore accommodates small-force, large-stroke actuators, as opposed to the current designs that use large-force, small-stroke actuators. The invention finds utility in numerous applications, including lightweight large aperture mirror substrate and RF reflector structures.
1. A deformable mirror assembly, comprising:
a substrate using a plurality of hinged beams to form a minimally rigid structure defining a two-dimensional surface;
the minimally rigid structure being characterized in that:
a) the structure is rigid, and
b) the removal of any one of the hinged beams permits relative motion between some points of the structure;
a face sheet physically coupled to the substrate; and
further including an actuator operative to command one or more of the beams to deform the face sheet.
2. The deformable mirror assembly of claim 1 , wherein the beams can be commanded to deform the face sheet in any manner, including tangential directions.
3. The deformable mirror assembly of claim 1 , wherein the actuator is a piezoelectric, electrostrictive or magnetostrictive device.
4. The deformable mirror assembly of claim 1 , wherein the structure is substantially ideal in the sense that the torque transmitted across any hinge is identically zero.
5. The deformable mirror assembly of claim 1 , wherein the structure made up of planar triangles, triangular pyramids or a combination thereof.
6. The deformable mirror assembly of claim 1 , wherein:
the face sheet is curved; and
the structure contains one of more gaps to avoid being over-constrained.
7. The deformable mirror assembly of claim 6 , wherein the face sheet is a paraboloid.
8. The deformable mirror assembly of claim 1 , wherein the face sheet is sufficiently thick or biased in tension to avoid compressive stresses.
9. The deformable mirror assembly of claim 1 , wherein the face sheet has a modulus of elasticity which is sufficiently low to maintain its shape during deformation.
10. The deformable mirror assembly of claim 1 , wherein the face sheet has a thickness of less than 0.10 mm.
11. The deformable mirror assembly of claim 1 , wherein the face sheet is a nano-laminate.
12. The deformable mirror assembly of claim 1 , wherein the face sheet is a membrane.
13. An optical mirror using the assembly of claim 1 .
14. An RF reflector using the assembly of claim 1 .
15. A method of deforming a mirror, comprising the steps of:
providing the assembly of claim 1 ; and
changing the length of one or more of the beams.
16. A deformable mirror, comprising:
a substrate using a plurality of hinged beams to form a minimally rigid structure defining a two-dimensional surface based upon planar triangles, triangular pyramids or a combination thereof;
the minimally rigid structure being characterized in that:
a) the structure is rigid, and
b) the removal of any one of the hinged beams permits relative motion between some points of the structure;
a face sheet physically coupled to the substrate; and
an actuator operative to command one or more of the beams to deform the face sheet.
17. The deformable mirror of claim 16 , wherein the beams can be commanded to deform the face sheet in any manner, including tangential directions.
18. The deformable mirror of claim 16 , wherein the actuator is a piezoelectric, electrostrictive or magnetostrictive device.
19. The deformable mirror of claim 16 , wherein the structure is substantially ideal in the sense that the torque transmitted across any hinge is identically zero.
20. The deformable mirror of claim 16 , wherein:
the face sheet is curved; and
the structure contains one of more gaps to avoid being over-constrained.
21. The deformable mirror of claim 20 , wherein the face sheet is a paraboloid.
22. The deformable mirror of claim 16 , wherein the face sheet is sufficiently thick or biased in tension to avoid compressive stresses.
23. The deformable mirror of claim 16 , wherein the face sheet has a modulus of elasticity which is sufficiently low to maintain its shape during deformation.
24. The deformable mirror of claim 16 , wherein the face sheet has a thickness of less than 0.10 mm.
25. The deformable mirror of claim 16 , wherein the face sheet is a nano-laminate.
26. The deformable mirror of claim 16 , wherein the face sheet is a membrane.